A study of longitudinal dynamic stability in flight (1924)
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236 REPORT NA^nOl^TALr ADVISORY COMIMITTEE PGR AERONAUTICS. Table II. H. and falls to a value of 1.25 at 70 and 95 The damping is a maximum of 0.70 at 83 M. P< with an increase in airspeed above a certain M. P. H., again showing that the damping decreases the locked control curves is given in Table… … Airspeed in MJiH. Airspeed in M.RH. Fig. 11.—VE-7 with free controls. Fig. 12.—JN41i with free controls. beloW; but it will be seen that the agreement with the observed values is not as good as it was fur the period. Table III. In Figure 12 arc shomi the free control characteristics of the…
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